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Re-Computation of Numerical Results Contained in NACA Report No. 741This paper presents recomputed theoretical results and compares those results with original results contained in NACA Report No. 741 (NACA 741), “Flutter Calculations in Three Degrees of Freedom,” by Theodore Theodorsen and I.E. Garrick. The recomputations were performed employing the solution method described in NACA 741 but using modern computational tools. With some exceptions, the magnitudes and trends of the original results were in good-to-excellent agreement with the recomputed results, a surprising but gratifying result considering that the NACA 741 results were computed “by hand” using pencil, paper, slide rules, and mechanical calculators called comptometers. Checks on the recomputations (about 25% to 30% were checked) were performed using the so-called k-method of flutter solution. In all cases, including those where the original and recomputed results differed significantly, the checks were in excellent agreement with the recomputed results.
Document ID
20230010473
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Boyd Perry
(Distinguished Research Associates Hampton, Virginia, United States)
Date Acquired
July 17, 2023
Publication Date
December 1, 2023
Subject Category
Aerodynamics
Report/Patent Number
NASA/TP-2015-218765
NASA/TP-2020-220562
Funding Number(s)
WBS: 981698.01.01.23.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Numerical results
recomputation
aeroelasticity
flutter
Theodorsen
Garrick
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